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公开(公告)号:DK136583D0
公开(公告)日:1983-03-25
申请号:DK136583
申请日:1983-03-25
Applicant: UNITED TECHNOLOGIES CORP
Inventor: HARNER KERMIT IVAN , KOS JOSEPH MICHAEL , PATRICK JOHN PETER
Abstract: An accelerometer (1) disposed on the support tower (12) of a wind turbine electric generating system in the vicinity of the rotor (10, 16) thereof provides a signal (1) indicative of acceleration of the tower in the direction of the rotor rotational axis. The signal (2) is passed through a band-pass filter (4) for summation (9) with a torque/power controlled (100) blade pitch angle reference rate signal (98), the integral (104) of which provides a blade pitch angle reference signal (40) to control the pitch angle of the rotor blades (10) through a pitch change mechanism (38), thereby to provide additional, positive aerodynamic damping to the tower while modulating blade angle for constant torque/power in response to wind turbulence.
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公开(公告)号:AU526931B2
公开(公告)日:1983-02-10
申请号:AU4963079
申请日:1979-08-07
Applicant: UNITED TECHNOLOGIES CORP
Inventor: KOS JOSEPH MICHAEL , PATRICK JOHN PETER , HARNER KERMIT IVAN
Abstract: A multi-mode electronic wind turbine control system establishes a reference blade angle BR for a two-bladed, horizontal axis, variable pitch wind turbine rotor, the blade angle being regulated by a hydraulic pitch change mechanism (38). The rotor (10), via appropriate shafts and a gearbox (20), is coupled to a synchronous generator (24) to produce electrical energy which is fed to a power utility grid. The control system (36) provides closed loop pitch control for rotor acceleration rate during start-up, for rotor deceleration rate during shut-down, for speed control when the synchronous generator is off-line, and for power control when the synchronous generator is on-line. A single control integrator is used for all closed loop operating modes, with a rate limiter circuit in front of the control integrator to prevent integrator overtravel. The integrator has maximum and minimum blade angle stops, the minimum stop being variable as a function of rotor speed and wind speed. When on-line, power control is provided by a unique shaft torque control using proportional plus integral plus derivative controls in combination.
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公开(公告)号:IT8026145D0
公开(公告)日:1980-11-21
申请号:IT2614580
申请日:1980-11-21
Applicant: UNITED TECHNOLOGIES CORP
Inventor: PATRICK JOHN PETER , GOODMAN ROBERT BERNARD
IPC: G05D23/00 , F24F3/052 , G05D23/13 , G05D23/185 , G01K
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公开(公告)号:FI76867B
公开(公告)日:1988-08-31
申请号:FI814151
申请日:1981-12-23
Applicant: UNITED TECHNOLOGIES CORP
Inventor: PATRICK JOHN PETER , KOS JOSEPH MICHAEL , HARNER KERMIT IVAN
Abstract: A blade pitch angle control for a wind turbine-generator establishing an optimum power or torque reference signal which, when operating conditions so warrant, is not limited by the nominal torque or power ratings of various turbine generator components. The reference signal is indicative of a maximum blade angle setting for safe operation of the wind turbine. An integral or lag compensation circuit for enhanced transient and steady-state operation may be employed.
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公开(公告)号:FI76627B
公开(公告)日:1988-07-29
申请号:FI792440
申请日:1979-08-06
Applicant: UNITED TECHNOLOGIES CORP
Inventor: KOS JOSEPH MICHAEL , PATRICK JOHN PETER , HARNER KERMIT IVAN
Abstract: A multi-mode electronic wind turbine control system establishes a reference blade angle BR for a two-bladed, horizontal axis, variable pitch wind turbine rotor, the blade angle being regulated by a hydraulic pitch change mechanism (38). The rotor (10), via appropriate shafts and a gearbox (20), is coupled to a synchronous generator (24) to produce electrical energy which is fed to a power utility grid. The control system (36) provides closed loop pitch control for rotor acceleration rate during start-up, for rotor deceleration rate during shut-down, for speed control when the synchronous generator is off-line, and for power control when the synchronous generator is on-line. A single control integrator is used for all closed loop operating modes, with a rate limiter circuit in front of the control integrator to prevent integrator overtravel. The integrator has maximum and minimum blade angle stops, the minimum stop being variable as a function of rotor speed and wind speed. When on-line, power control is provided by a unique shaft torque control using proportional plus integral plus derivative controls in combination.
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公开(公告)号:NO156257C
公开(公告)日:1987-08-19
申请号:NO814360
申请日:1981-12-21
Applicant: UNITED TECHNOLOGIES CORP
Inventor: PATRICK JOHN PETER , KOS JOSEPH MICHAEL , HARNER KERMIT IVAN
Abstract: A blade pitch angle control for a wind turbine-generator establishing an optimum power or torque reference signal which, when operating conditions so warrant, is not limited by the nominal torque or power ratings of various turbine generator components. The reference signal is indicative of a maximum blade angle setting for safe operation of the wind turbine. An integral or lag compensation circuit for enhanced transient and steady-state operation may be employed.
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公开(公告)号:IN158792B
公开(公告)日:1987-01-24
申请号:IN700CA1983
申请日:1983-06-02
Applicant: UNITED TECHNOLOGIES CORP
Inventor: HARNER KERMIT IVAN , PATRICK JOHN PETER , VOSSELLER KENNETH FRANKLYN
Abstract: A blade feathering system for wind turbines includes a feather actuator (299), control means (330 and 335) operatively connected thereto and an adjustment means (340) operatively connected to the control means for selectively varying the rate of operation of the feather actuator for feathering the wind turbine blades (10 and 15) at a variable rate.
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公开(公告)号:IN158212B
公开(公告)日:1986-09-27
申请号:IN321CA1983
申请日:1983-03-16
Applicant: UNITED TECHNOLOGIES CORP
Inventor: KOS JOSEPH MICHAEL , PATRICK JOHN PETER , HARNER KERMIT IVAN
Abstract: An accelerometer (1) disposed on the support tower (12) of a wind turbine electric generating system in the vicinity of the rotor (10, 16) thereof provides a signal (1) indicative of acceleration of the tower in the direction of the rotor rotational axis. The signal (2) is passed through a band-pass filter (4) for summation (9) with a torque/power controlled (100) blade pitch angle reference rate signal (98), the integral (104) of which provides a blade pitch angle reference signal (40) to control the pitch angle of the rotor blades (10) through a pitch change mechanism (38), thereby to provide additional, positive aerodynamic damping to the tower while modulating blade angle for constant torque/power in response to wind turbulence.
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公开(公告)号:NO153470C
公开(公告)日:1986-04-02
申请号:NO803517
申请日:1980-11-21
Applicant: UNITED TECHNOLOGIES CORP
Inventor: PATRICK JOHN PETER , GOODMAN ROBERT BERNARD
IPC: G05D23/00 , F24F3/052 , G05D23/13 , G05D23/185
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公开(公告)号:GB2117933B
公开(公告)日:1985-07-31
申请号:GB8305992
申请日:1983-03-04
Applicant: UNITED TECHNOLOGIES CORP
Inventor: KOS JOSEPH MICHAEL , PATRICK JOHN PETER , HARNER KERMIT IVAN
Abstract: An accelerometer (1) disposed on the support tower (12) of a wind turbine electric generating system in the vicinity of the rotor (10, 16) thereof provides a signal (1) indicative of acceleration of the tower in the direction of the rotor rotational axis. The signal (2) is passed through a band-pass filter (4) for summation (9) with a torque/power controlled (100) blade pitch angle reference rate signal (98), the integral (104) of which provides a blade pitch angle reference signal (40) to control the pitch angle of the rotor blades (10) through a pitch change mechanism (38), thereby to provide additional, positive aerodynamic damping to the tower while modulating blade angle for constant torque/power in response to wind turbulence.
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